| A/C | Manufacturer | BAe | Sources: | |||
| Aircraft type | Jetstream 31/32 | [1] | https://www.flightglobal.com/download?ac=73559 | |||
| Total number of operating A/C | 101 | [1] | [2] | https://www.easa.europa.eu/downloads/8171/en | ||
| Option/Variant | 32 | [2] | [3] | https://www.globalair.com/aircraft-for-sale/Specifications?specid=849 | ||
| Engine | No. of Engines | 2 | [2] | [4] | https://www.bfu-web.de/EN/Publications/Interim_Reports/IR2019/IR1_19-1422-EX_BAE-JS32_Muenster-Osnabr.pdf?__blob=publicationFile | |
| Model | TPE 331-12UHR | [2] | ||||
| Max. Rated Takeoff Thrust, T_TO [kN] | - | |||||
| Equivalent Power, P [kW] | 750 | [2] | ||||
| Propeller | R.333/4-82-F/12 | [2] | ||||
| Cabin | Length, l_CABIN [m] | 7,39 | [3] | |||
| Max. Height, h_CABIN [m] | 1,6 | [3] | ||||
| Max. Width, d_F,I [m] | 1,91 | [3] | ||||
| Passenger Compartment Volume, V_CABIN [m³] | 17 | [3] | ||||
| Fuselage | Height, h_F [m] | 1,98 | [4] | |||
| Width, w_F [m] | 1,98 | [4] | ||||
| Total | Length, l_A/C [m] | 14,36 | [2] | |||
| Span, b_W [m] | 15,85 | [2] | ||||
| Height, h_A/C [m] | 5,2 | [2] | ||||
| Landing Gear | Track, l_T [m] | 5,94 | [2] | |||
| Wheelbase, l_WB [m] | 4,6 | [2] | ||||
| Wing | Area, S_W [m²] | 25,08 | [2] | |||
| Taper ratio, λ_W | 0,33 | [4] | ||||
| 1/4 Chord Sweep, φ_25,W [°] | 0,7 | [4] | ||||
| Vertical Tail | Area, S_V [m²] | N/A | ||||
| Height, b_V [m] | 3,2 | [4] | ||||
| Taper ratio, λ_V | 0,295 | [4] | ||||
| 1/4 Chord Sweep, φ_25,V [°] | 40 | [4] | ||||
| Horizontal Tail | Area, S_H [m²] | N/A | ||||
| Span, b_H [m] | 6,6 | [4] | ||||
| Taper Ratio, λ_H | 0,41 | [4] | ||||
| 1/4 Chord Sweep, φ_25,H [°] | 7,12 | [4] | ||||
| Cruise | V_MO [kt] | 250 | [3] | |||
| M_MO [Mach] | - | |||||
| Cruise Speed, M_CR [Mach] | 210 | [3] | ||||
| Max. Certified Flight Level, h_MCR [FL] | 250 | [2] | ||||
| Cruise Altitude, h_CR [FL] | N/A | |||||
| Fuel | Unusable Fuel [l] | 18 | [2] | |||
| Optional Fuel [l] | - | |||||
| Max usable fuel [l] | 1846 | [2] | ||||
| Range | Max. Payload, R_MPL [nm] | N/A | ||||
| Max. Pax, R_M,pax [nm] | N/A | |||||
| Max. Range, R_PLMR [nm] | N/A | |||||
| Mass | Max. Ramp, m_MR (MRM) [kg] | 7400 | [2] | |||
| Max. Take-Off, m_MTO (MTOM) [kg] | 7350 | [2] | ||||
| Max. Landing, m_ML (MLM) [kg] | 7080 | [2] | ||||
| Max. Zero Fuel, m_MZF (MZFM) [kg] | 6736 | [2] | ||||
| Operating Empty, m_OE (OEM) (MZFM-MPL) [kg] | 5098 | |||||
| Max. Payload, m_MPL (MPL) [kg] | 1638 | [3] | ||||
| Payload at Max. Range, m_PLMR [kg] | N/A | |||||
| Cargo | Volume, V_CARGO [m³] | 0,45 | [3] | |||
| Cargo Capacity | - | |||||
| Max. Pallet Underfloor | - | |||||
| Seats | Max. Seats, n_M,SEAT | 19 | [2] | |||
| Std. Layout, n_SEAT | 19 | [3] | ||||